Robust reliable gain scheduling control for helicopters

Author

Jiao, Yusong ; Wang, Xinmin ; Yu, Xiang

Author_Institution

Sch. of Autom., Northwestern Polytech. Univ., Xi´´an

fYear

2008

fDate

1-3 Sept. 2008

Firstpage

1721

Lastpage

1724

Abstract

This paper is concerned with the problem of robust reliable gain-scheduled state feedback controller design for rotorcraft dynamic systems with multiple operating points. Based on parameter dependent Lyapunov function approach and parameter dependent multipliers technique, the construction of reliable H₂ gain-scheduled helicopter flight controllers via state feedback is developed in terms of solutions to a set of linear matrix inequalities (LMIs).

Keywords

Lyapunov methods; aerospace control; control system synthesis; gain control; helicopters; linear matrix inequalities; robust control; scheduling; state feedback; H₂ gain-scheduled helicopter; flight controller; linear matrix inequality; parameter dependent Lyapunov function approach; parameter dependent multiplier technique; robust reliable gain scheduling control; rotorcraft dynamic system; state feedback controller design; Actuators; Control systems; Design automation; Helicopters; Linear matrix inequalities; Lyapunov method; Robust control; Scheduling; State feedback; Uncertainty; Gain scheduling; Helicopter; Robust control. Reliable control;

fLanguage

English

Publisher

ieee

Conference_Titel

Automation and Logistics, 2008. ICAL 2008. IEEE International Conference on

Conference_Location

Qingdao

Print_ISBN

978-1-4244-2502-0

Electronic_ISBN

978-1-4244-2503-7

Type

conf

DOI

10.1109/ICAL.2008.4636433

Filename

4636433